ATLAS 5 CENTAUR DEB, 43958

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 43958 is space debris in HEO originally from a launch on Wed, 17 Sep 2014 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
43958, 2014-055M
Orbit
HEO
Last TLE update
1 week ago
Origin
Flag of USUnited Launch Alliance/Lockheed Martin (US)
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2014-09-17 (11 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history

TLE from 1 week ago
0 ATLAS 5 CENTAUR DEB
1 43958U 14055M   25193.32157232 -.00000021  00000-0  00000+0 0  9992
2 43958  19.8445 168.8198 4774131 121.6823 293.6961  1.89316005 47452
Epoch: 2025-07-12T07:43Z
TLE epoch observation values (Epoch: 2025-07-12T07:43:03.848Z)
Latitude
-0.00003°
Longitude
122.53265°
Altitude
22,058.439 km
Speed
3.687 km/s
True Right ascension
11h 15m 02s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-18.20099°
Longitude
56.35637°
Altitude
33,893.982 km
Speed
2.314 km/s
Apparent Right ascension
06h 20m 55s
Apparent Declination
-23° 35' 26"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:28:06
Azimuth
252.518° W
Elevation
-16.192°
Doppler factor
1
Orbital elements
Apogee altitude
34,404.607 km
Perigee altitude
8,047.434 km
Semi-major axis
27,604.157 km
Eccentricity
0.47741
Inclination
19.8445°
RAAN
168.8198°
Arg. of periapsis
121.6823°
True anomaly
238.36363°
Mean anomaly
293.6961°
Eccentric anomaly
266.39643°
Mean motion
0.47324 °/min
Orbital period
760.71 mins
BSTAR
0
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